Method for actively isolating angular vibration of optical system of full-strapdown seeker

An optical system and active vibration isolation technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve the problem of less research on angular vibration isolation design, adverse effects of missile strike accuracy, isolation of lateral vibration and longitudinal vibration Imperfect design and other issues

Inactive Publication Date: 2013-09-25
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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Problems solved by technology

[0004] At present, the vibration isolation design of the full strapdown seeker mostly focuses on the vibration isolation of the linear vibration along the optical axis (also called longitudinal vibration) through the passive vibration isolation strategy, and a small number of scholars also focus on the vibration perpendicular to the optical axis (also known as longitudinal vibration). known as lateral vibration) for vibration isolation design, but less research on diagonal vibration isolation design
In addition, the imperfect isolation design of lateral vibration and longitudinal vibration often introduces coupled angular vibration, which adversely affects the strike accuracy of missiles

Method used

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  • Method for actively isolating angular vibration of optical system of full-strapdown seeker
  • Method for actively isolating angular vibration of optical system of full-strapdown seeker
  • Method for actively isolating angular vibration of optical system of full-strapdown seeker

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Embodiment

[0057] Select a missile full strapdown optical system, its moment of inertia is J=9.3×10 -4 kgm 2 , the distance between the center of the spherical joint 1 and the action point of the spring damper 6 along the optical axis is r=0.06m; the maneuvering frequency of the missile is 20Hz, when f≤20Hz, the angular vibration transmission efficiency is required |1-TR|≤3 %; when f≥30Hz, the angular vibration transmittance TR≤70.1% is required (that is, the transmittance is less than -3db).

[0058] In this embodiment, the center of mass of the optical system 2 is located at the center of the spherical joint 1 by adopting a mechanical design method, thereby avoiding the coupling effect caused by the unbalanced mass on the vibration. Then according to the requirements of the system transmissibility, through calculation, the natural angular frequency of the system is selected as ω n =161.5rad / s, the stiffness of spring 6 is k=6.74×10 3 N / m, the approximate damping value of Sky-Hook da...

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Abstract

The invention discloses a method for actively isolating angular vibration of an optical system of a full-strapdown seeker, and relates to the field of vibration isolation technologies for optical systems of full-strapdown seekers. The method has the advantages that the optical system is connected with a guided missile body by a spherical hinge, the mass center of the optical system is coincided with the center of the spherical hinge by the aid of a design, and accordingly the coupled angular vibration is prevented from being led into structural linear vibration; a Sky-Hook damping model is constructed, so that angular vibration response and angular vibration excitation are integrated into the classic Sky-Hook model, and proper spring stiffness and a proper damping value can be selected according to the requirement of the system on a vibration isolation effect; the angular vibration isolation can be actively controlled, so that the guided missile body is excited by the angular vibration, the angular vibration response of the optical system is good in attitude reproducibility in a maneuvering frequency band of a guided missile, and the vibration can be effectively isolated in a noise and vibration frequency band.

Description

technical field [0001] The invention relates to the technical field of vibration isolation of the optical system of a strapdown seeker, in particular to an active vibration isolation method for the angular vibration of the optical system of a strapdown seeker based on a Sky-Hook damping model. Background technique [0002] There are many traditional seeker platform stabilization methods, including dynamic gyro stabilization, integral gyro stabilization, and rate gyro stabilization. The most commonly used is the seeker stabilized platform with a rate gyro. The angular rate sensor installed on the seeker stabilized platform directly transmits the signal to the torque motor to provide stability compensation. With the development of high-precision inertial integrated navigation technology and the progress of high-performance microprocessors, strapdown seeker guidance and its digital control technology have become an important research direction for small, fast and low-cost seeke...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
Inventor 孙辉关永亮刘波贾宏光
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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